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Space Shuttle with rail system and aft thrust structure securing solid rocket boosters to external tankThe configuration and relationship of the external propellant tank and solid rocket boosters of space transportation systems such as the space shuttle are described. The space shuttle system with the improved propellant tank is shown. The external tank has a forward pressure vessel for liquid hydrogen and an aft pressure vessel for liquid oxygen. The solid rocket boosters are joined together by a thrust frame which extends across and behind the external tank. The thrust of the orbiter's main rocket engines are transmitted to the aft portion of the external tank and the thrust of the solid rocket boosters are transmitted to the aft end of the external tank.
Document ID
19840019715
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Vonpragenau, G. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
June 5, 1984
Subject Category
Space Transportation
Report/Patent Number
Patent Number: NASA-CASE-MFS-25853-1
Patent Number: US-PATENT-4,452,412
Patent Application Number: US-PATENT-APPL-SN-418138
Accession Number
84N27784
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MFS-25853-1|US-PATENT-4,452,412
Patent Application
US-PATENT-APPL-SN-418138
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